{
  "$type": "site.standard.document",
  "description": "In a gas turbine engine 101 of the type having a high-pressure (HP) spool and a low-pressure (LP) spool, methods of increasing surge margin and compression efficiency at a given thrust are provided. One method increases compression efficiency and comprises transferring mechanical power from the HP…",
  "path": "/patents/1434410",
  "publishedAt": "2024-05-29T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D15/10",
    "ROLLS ROYCE PLC [GB]"
  ],
  "textContent": "In a gas turbine engine 101 of the type having a high-pressure (HP) spool and a low-pressure (LP) spool, methods of increasing surge margin and compression efficiency at a given thrust are provided. One method increases compression efficiency and comprises transferring mechanical power from the HP spool to the LP spool to reduce a corrected speed of a HP compressor 105 therein and raise a working line of a LP compressor 104 therein. Another method increases surge margin and comprises transferring mechanical power from the LP spool to the HP spool to increase a corrected speed of a HP compressor 105 therein and lower a working line of a LP compressor 104 therein.",
  "title": "INCREASING COMPRESSION EFFICIENCY VIA SHAFT POWER TRANSFER"
}